GB600370A - Turbine unit - Google Patents

Turbine unit

Info

Publication number
GB600370A
GB600370A GB2463445A GB2463445A GB600370A GB 600370 A GB600370 A GB 600370A GB 2463445 A GB2463445 A GB 2463445A GB 2463445 A GB2463445 A GB 2463445A GB 600370 A GB600370 A GB 600370A
Authority
GB
United Kingdom
Prior art keywords
injection nozzle
nozzle
turbine unit
chamber
leitch
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB2463445A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WILLIAM RICHARDS LEITCH
Original Assignee
WILLIAM RICHARDS LEITCH
Filing date
Publication date
Application filed by WILLIAM RICHARDS LEITCH filed Critical WILLIAM RICHARDS LEITCH
Publication of GB600370A publication Critical patent/GB600370A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)

Abstract

600,370. Gas turbines. LEITCH, W. R. Sept. 24, 1946, No. 24634/45. [Class 110 (iii)] [Also in Group XII] The combustion chamber 1 is fitted with a fuel injection nozzle 2, an air injection nozzle 3 and a water injection nozzle 4, the nozzles 2 and 3 being so relatively inclined that their produced centre lines intersect one another within the chamber and the nozzle 4,being so disposed that its discharge end is upstream of the point of intersection. The mixture of combustion gases and steam passes through ducts 5 to the turbine wheel 6.
GB2463445A 1946-09-24 Turbine unit Expired GB600370A (en)

Publications (1)

Publication Number Publication Date
GB600370A true GB600370A (en) 1948-04-07

Family

ID=1738533

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2463445A Expired GB600370A (en) 1946-09-24 Turbine unit

Country Status (1)

Country Link
GB (1) GB600370A (en)

Similar Documents

Publication Publication Date Title
GB650462A (en) Improvements in or relating to combustion apparatus
GB588847A (en) Improvements in combustion chambers for internal combustion turbines
GB904142A (en) Improvements in or relating to gas-turbine engines
GB579424A (en) Improvements relating to liquid fuel combustion apparatus for generating gases for power purposes
GB818634A (en) Improvements in or relating to combustion chambers for gas turbines
GB587083A (en) Improvements in combustion chambers for internal combustion turbines
GB657789A (en) Improvements relating to liquid fuel combustion equipment for gas-turbine engines
GB649500A (en) Improvements in or relating to fuel combustion apparatus
GB757332A (en) Liquid fuel combustion chambers for jet-propulsion, engines, gas turbines, or other purposes
GB922069A (en) Combustion chamber for a gas turbine engine
GB669751A (en) Improvements relating to combustion chambers for gas turbine plants and the like
GB654122A (en) Improvements in or relating to combustion equipment for gas-turbine engines
GB1524217A (en) Combustion chamber for a gas turbine engine
GB600370A (en) Turbine unit
GB648699A (en) Improvements in or relating to gas-turbine engine fuel systems and liquid fuel injectors therefor
GB565952A (en) Improvements in means for generating a mixture of steam and combustion products under pressure
GB674641A (en) Fuel-burning means for a gaseous-fluid propulsion jet
GB619353A (en) Liquid-fuel combustion chamber
GB679145A (en) Improvements in combustion apparatus
GB885908A (en) Improvements in intakes for compressible fluids
GB682778A (en) Improvements relating to combustion chambers for prime movers
GB618644A (en) Improvements in or relating to combustion units
GB702752A (en) Improvements relating to combustion equipment of gas turbine engines
GB620073A (en) Improvements in or relating to combustion systems for gas turbines with heat exchangers
GB670968A (en) Vapourizing system for a gas turbine engine